· The effects of the complex
stresses in a symmetric cross-ply laminate are illustrated. · As a result of an applied longitudinal stress
on the laminate, the central lamina cracks in the direction parallel to its
fibers. · The interactions between
the laminae can increase the transverse tensile stress on the outer longitudinal
laminae until they fracture parallel to their fibers.
From:
Hull, "Introduction to Composite Materials," Cambridge (1992)